Cross coil type indicator

ABSTRACT

In a cross coil type indicator having a pair of cross coils arranged in quadrature, a magnet rotor having a shaft and a pointer attached to the shaft and rotatably positioned within the coils, the pointer is positioned to indicate a variable by flowing pulse currents through the coils in which the duty ratio is related to the variable value. Digital data corresponding to the pointer angle is stored as sin or cos θ data in a memory such as a read only memory (ROM) to enable simple calculation of pointer position from the duty ratio of the current pulse. The configuration disclosed requires only a minimum memory size. The need for extra memory capacity is minimized by storing, within a sin θ and cosine θ generating means, only sin θ data within the range of φ°≦θ≦90°.

This is a continuation of co-pending application Ser. No. 07/389,880 filed on Aug. 4, 1989, now U.S. Pat. No. 5,119,320.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to a cross coil type indicator in which a magnet rotor is rotated by a resultant magnetic field generated by cross coils arranged in quadrature with each other and a detected variable is indicated by a pointer rotated together with the rotor.

2. Description of the Prior Art

As shown in FIG. 1, the pointer driving portion of the cross coil type indicator is, in general, comprised of a pair of coils L₁ and L₂ arranged in quadrature with each other, a magnet rotor Mg rotatively provided in a resultant magnetic field generated by the two coils L₁ and L₂, a pointer A provided at one end of the rotary shaft (not shown) mounted on the magnet rotor Mg, a scale plate B for indicating the detected variable in cooperation with the rotating position of the pointer A, a zero point stopper pin P which restricts the rotation of the pointer A, and a spiral spring C for biasing the pointer A and the magnet rotor Mg toward the stopper pin P.

With this construction, when drive currents i₁ and i₂ are flowed through the cross coils L₁ and L₂ in quadrature as shown in FIG. 2, respectively, magnetic fields generated in each of the coils can be represented by the following equations; ##EQU1##

Here, μ₁ and μ₂ indicate each magnetic permeability of the coils L₁ and L₂, respectively,

n₁ and n₂ indicate the number of windings of the coils, respectively, and

S₁ and S₂ indicate each cross-sectional area of the coils, respectively.

On the other hand, since the magnet rotor Mg is rotated in the resultant magnetic direction of the magnetic fields φ₁ and φ₂, its rotation angle α can be represented by the following equation; ##EQU2##

When the coils L₁ and L₂ having an equal structure respectively is used, the equation (2) can be rewritten as follows; ##EQU3##

That is to say, the rotation angle α is defined by the drive currents i₁ and i₂.

Supposing that the drive currents i₁ and i₂ are ##EQU4## then, the rotation angle θ corresponding to the resultant magnetic field can be represented as follows; ##EQU5##

Namely, the rotation angle θ becomes equal to the rotation angle of the pointer, i.e., α=θ. As a result, the direction of the resultant magnetic field generated by the cross coils L₁ and L₂ becomes equal to the angle 8 as shown in FIG. 3 and the magnet rotor Mg is rotated up to the rotation angle θ against the biasing force of the spiral spring C, which corresponds to the detected variable.

Accordingly, by reading the position of the pointer A which rotates together with the magnet rotor Mg with respect to the scale plate B, it becomes possible to know the value of the detected variable. It is to be noted that the amplitudes of the drive currents i₁ and i₂ in this case are determined by taking into consideration of the biasing force of the spiral spring C.

In order to drive the cross coils as set forth above, it is necessary to provide a drive unit for driving the cross coils. In this case, it is preferable for the drive unit to be able to apply pulse currents of sin θ and cos θ having duty ratios corresponding to the detected variable to the cross coils as the drive currents. Further, in order to lower production cost of the indicator, it is requested for the drive unit to have a simple structure. Furthermore, if there is provided such a drive unit in an cross coil type indicator, several problems caused in a conventional cross coil type indicator can be settled since it becomes possible to make degital processing of various data.

Hereinafter, one of the problems will be described with reference to the drawings.

FIGS. 4 to 6 show one of prior art indicators having a drive unit which can apply pules currents having duty ratios corresponding to the detected variable.

Namely, in the drive unit of the cross coil type indicator as shown in FIG. 4, pulse currents having duty ratios corresponding to the detected variable are generated, and they are applied to the cross coils L₁ and L₂ through an output circuit 50.

The drive unit comprises a sensor 10 for detecting a variable such as car speed, a frequency/voltage (F/V) converter 20, a duty ratio calculating circuit 30, a duty pulse generating circuit 40 and an output circuit 50. The cross coils L₁ and L₂ and the magnet rotor Mg are the same as those indicated in FIG. 1.

In operation, an output signal such as vehicle speed from the sensor 10 is applied to the frequency/voltage (F/V) converter 20, where the frequency of the output signal is converted into a D.C. voltage. The D.C. voltage thus converted is applied to a duty ratio calculating circuit 30, where sin θ and cos θ of the rotation angle 0 of the pointer A are sought in accordance with the voltage. Then, each duty ratio shown in FIG. 5 is calculated therein from duty characteristics which change in accordance with sin θ and cos θ. Each of the duty pulses is generated in the duty pulse generating circuit 40 and pulse currents having duty ratios are applied to the coils L₁ and L₂ through the output circuit 50, respectively.

Since the pulse currents i₁ and i₂ are proportional to sin θ and cos θ and the angle α of the resultant magnetic field is changed in accordance with the detected variable, the pointer A is rotated against the biasing force of the spiral spring in the direction of the resultant magnetic field vector, thus enabling the read-out of the rotation angle of the pointer A from the scale plate B.

Now, as stated previously a stopper pin P is provided at a position near the zero indicating position as shown in FIG. 1 and the pointer A is normally biased by the spiral spring C toward the stopper pin P. As a result, when the pointer A is situated near the zero indicating position in the case of a speed meter or "E" position in the case of a fuel indicator, the pointer A comes into contact with the stopper pin P. Since a desirable linearity in indication cannot be maintained in the vicinity of "zero" or "E" position on the scale plate B, the "zero" or "E" position has to be shifted to a higher position which is normally about 5° to 10° above from its actual position, and the stopper pin position must also be shifted to the corresponding position. Because of this situation, noise is generated by repeated abutments between the pointer and stopper pin due to the reasons which will be explained later.

FIG. 6 indicates a detailed circuit construction of the output circuit 50 shown in FIG. 4. In the output circuit 50, two pairs of the NPN transistors Q11, Q13 and Q12, Q14 are connected in the form of a first bridge circuit together having the first coil L₁, and another two pairs of the NPN transistors Q21, Q23 and Q22, Q24 are connected in the form of a second bridge circuit having the second coil L₂ between the power supply +Vcc and the ground. Each base of the transistors Q11 through 24 is connected to the duty pulse generating circuit 40.

In operation, when each of the pulse currents i₁ and i₂ is desired to flow through the coils L₁ and L₂ in the direction of the solid line shown in FIG. 6, the transistors Q11, Q14 are turned on and the transistors Q21, Q24 are turned off, while the transistors Q21, Q24 are turned on and the transistors Q22, Q23 are turned off by the application of pulse signals to the base of each transistor from the duty pulse generating circuit 40.

On the other hand, when the pulse currents i₁ and i₂ as the drive currents are desired to flow through the coils L₁ and L₂ in the direction of the dotted line shown in FIG. 6, the transistors Q12, Q13 are turned on and the transistors Q11, Q14 are turned off while the transistors Q22, Q23 are turned on and the transistors Q21, Q24 are turned off.

Since the pointer A is driven by the pulse currents flowing through the coils L₁ and L₂, which are responsive to the changes in the duty ratios or the detected variable, the pointer A is subject to a vibration generated by the changes and therefore noise is generated when the pointer A strikes the stopper pin P. Especially, when the indicator is applied to a speed meter, under the low speed condition the pointer A is constructed in such a manner that it never comes off from the stopper pin so that on and off action is repeatedly happened between the pointer A and the stopper pin P at a low speed condition due to the vibration in the changes of the detected variable, and noise is generated thereby.

SUMMARY OF THE INVENTION

It is therefore a first object of the present invention to provide a cross-coil type indicator having a drive unit for driving cross coils, which has a simple structure so as to produce it with low cost.

It is a second object of the present invention to provide a cross-coil type indicator in which the duty ratios of pulse currents are calculated by digital data corresponding to rotational angles θ of the pointer of the indicator, and its sin θ and cos θ, which have been preliminarily stored in a ROM and read from the ROM, and pulse currents having each duty ratios responsive to a detected variable are generated in a duty pulse generating circuit and they are applied to cross coils in quadrature, thereby simplifying the duty ratio calculation.

It is a third object of the present invention to provide a cross coil type indicator having a stopper pin for restricting the rotational movement of a pointer of the indicator in which detection means for detecting whether or not actual rotational angles of the pointer of the indicator fall within a predetermined range of angles and for producing an output signal in accordance with the result of the detection, and compensation means for compensating the duty ratios of the pulse currents to be applied to the cross coils are provided, whereby only when the actual rotational angle of the pointer falls within the predetermined range of angle, the compensation means compensates for the duty ratios of the pulse currents, so as to reduce the torque of the pointer and to suppress the generation of noise caused by repeated abutments between the pointer and the stopper pin.

In order to achieve the first and second objects, a cross coil type indicator having a drive unit includes a pair of cross coils arranged in quadrature, and a magnet rotor having a pointer at its center and rotatively provided within the coils by a resultant magnetic field generated by the coils and capable of indicating a detected variable by flowing pulse currents in the coils in accordance with the detected variable, wherein the indicator further comprises: data generating means for generating sin θ and cos θ data in accordance with the actual rotational angle of the pointer responsive to the detected variable, a ROM forming the data generating means; pulse generating means for generating pulse currents having duty ratios corresponding to the sin θ and cos θ thus generated and to be applied to the cross coils; and output circuit means for driving the coils in accordance with the pulse currents thus generated.

According to the cross coil type indicator with a drive unit having the above structure, data processing is performed in the single ROM forming the data generating means, it becomes possible to simplify its structure, thus leading to a reduction in manufacturing cost. Further, according to this cross coil type indicator, since only sin θ data within the range of 0° θ≦90° is to be stored in the ROM, it becomes possible to have high resolutional indication characteristic by a ROM having a certain capacity in comparison with the cases in which the other data is stored therein.

Further, in order to achive the third object, a cross coil type indicator of the present invention includes a pair of cross coils arranged in quadrature, a magnet rotor having a pointer at its center and rotatively provided within the coils by a resultant magnetic field generated by the cross coils and capable of indicating a detected variable by flowing pulse currents in the coils in accordance with the detected variable and a stopper pin for restricting the movement of the pointer at a low rotational angle, wherein the indicator further comprises: detection means for detecting whether or not actual rotational angles of the pointer of the indicator fall within a predetermined range of angle, where the pointer has a possibility of contacting with the stopper pin, and for providing an output signal in accordance with the result of the detection; and a current control circuit means having its input connected to the output of the detection and its output thereof connected to an output circuit means for driving the cross coils by pulse currents having duty ratios calculated by a duty ratio calculation circuit means, whereby only when the former angle of the pointer is within the predetermined latter angle, the amplitudes of the pulse currents from the output circuit means are reduced by an output signal from the current control circuit means.

According to the cross coil type indicator having the above structure, it becomes possible to suppress generation of noise caused by repeated abutments between the pointer and steer pin within the predetermined range of the angle of the pointer.

These objects, features, and advantages of the invention will be better understood from the following description with reference to the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows a basic construction of the cross coil type indicator having cross coils, a magnet rotor with a pointer, a bias spring and a scale plate, according to a prior art;

FIG. 2 shows the cross coils through which drive currents flow;

FIG. 3 shows a resultant magnetic field of the magnetic fields generated by the cross coils;

FIG. 4 shows a drive unit for the cross coils according to a prior art;

FIG. 5 shows the characteristics of duty ratios of sin θ and cos θ about the currents to be applied to the cross coils;

FIG. 6 shows a detailed description of the output circuit shown in FIG. 4;

FIG. 7 shows one example of a drive unit for a cross coil type indicator according to the present invention;

FIG. 8 shows the other embodiment of a drive unit for a cross coil type according to the present invention;

FIG. 9 shows the characteristics between pointer torque and rotational angle of the pointer;

FIG. 10 shows another embodiment of a drive unit for a cross coil type indicator according to the present invention;

FIG. 11 is a control flow chart of the microprocessor shown in FIG. 9;

FIG. 12 shows one embodiment of the output circuit and a current control circuit according to the present invention;

FIG. 13 shows still another embodiment of a drive unit for a cross coil type indicator according to the present invention;

FIG. 14 shows a further embodiment of a drive unit for a cross coil type indicator according to the present invention;

FIG. 15 shows the duty ratios of the currents without compensation;

FIG. 16 shows the compensated duty ratios of the currents to be applied to the cross coils; and

FIG. 17 is another control flow chart of the microprocessor shown in FIG. 14.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

Referring now to the accompanying drawings, preferred embodiments of the present invention will be described.

FIG. 7 shows an embodiment of a drive units for driving cross coils L₁ and L₂ by pulse currents of sin θ and cos θ generated by a sin θ function generator of a ROM.

The drive unit comprises a clock circuit 1, a counter circuit 2, a sin θ function generator circuit 3, a sin θ duty pulse generator 4, a cos θ duty pulse generator 5, a first drive circuit 6, a second drive circuit 7, and a direction setting circuit 8. The cross coils L₁ and L₂ arranged in quadrature with each other are constructed in the same manner as those indicated in FIG. 1.

In operation, a rectangular signal, the time period of which varies in accordance with the detected variable such as vehicle speed and clock signals are applied to the counter circuit 2. The output signal from the counter circuit 2 is applied to the sin θ function generator circuit 3 and the sin θ function signal from the function generator circuit 3 of a ROM is applied to sin θ duty pulse generator circuit 4 directly, so as to generate a sin θ duty pulse therefrom.

On the other hand, the sin θ function signal is indirectly applied to the cos θ duty pulse generator 5. Namely, the sin θ function signal from the function generator circuit 3 is applied to the drive circuit 7 after shifting the phase of the sin θ output signal by 90° by phase shift means (not shown) according to the principle of sin (90°+θ)=cos θ.

The pulse currents thus generated by the sin θ duty pulse generator 4 and cos θ duty pulse generator 5 are applied to the coils L₁ and L₂ through the drive circuits 6 and 7, respectively.

The direction setting circuit θ determines the direction of the drive currents flowing through the cross coils L₁ and L₂ in accordance with the output signal from the counter 2 circuit. The following table 1 indicates the relationship among the quadrant, angles, and the connection of the output terminals in the drive circuits 6, 7.

                  TABLE 1                                                          ______________________________________                                                                      OUTPUT                                            DIGITAL  QUAD-               TERMINALS                                         DATA     RANT     ANGLE      a.sub.1                                                                            a.sub.2                                                                              b.sub.1                                                                            b.sub.2                             ______________________________________                                          0-90    1         0°-90°                                                                     i.sub.1                                                                            G     i.sub.2                                                                            G                                    90-180  2         90°-180°                                                                   i.sub.1                                                                            G     G   i.sub.2                             180-270  3        180°-270°                                                                   G   i.sub.1                                                                              G   i.sub.2                             270-360  4        270°-360°                                                                   G   i.sub.1                                                                              i.sub.2                                                                            G                                   ______________________________________                                          Note) G indicates the ground level.                                      

As shown in the table 1, the output terminals a₁, a₂, b₁, and b₂ of the drive circuits 6 and 7 are selected in accordance with the digital data from the counter circuit 2. Since each of the currents i₁ and i₂ flowing through the coils correspond to sin θ and cos θ, the direction of the resultant magnetic field vector varies according to the detected variable. Accordingly, the magnet rotor Mg is rotated in the direction of the resultant magnetic field.

The sin θ function generator circuit 3 can be formed by a ROM. Each of the digital data corresponding to angle θ of sin θ data has preliminarily been stored in the ROM as shown in the following table 2.

                  TABLE 2                                                          ______________________________________                                         DIGITAL DATA   ANGLE θ°                                                                       sin θ                                                                           (cos θ)                               ______________________________________                                          0    180    180    360   0         0    1                                     .     .      .      .    .          .    .                                     .     .      .      .    .          .    .                                     .     .      .      .    .          .    .                                     30    150    210    230  30         0.5  0.85                                  .     .      .      .    .          .    .                                     .     .      .      .    .          .    .                                     .     .      .      .    .          .    .                                     90     90    270    270  90         1    0                                     ______________________________________                                    

Here, the angle θ corresponding to the degital data "0" is set to 0°, and rate of change of the degital data (in this table "1") corresponds to angle 1°, of which sin θ data is in the ROM. Further, the sin θ data has been stored within the range of 0°≦θ≦90° in the table 2. The sin θ data within the ranges of 90°≦θ≦180°, 180°≦θ≦270° and 270°≦θ≦360° are corresponding to the sin θ data within the range of 0°≦θ≦90°, respectively.

However, it is also possible to store the sin θ data between 0°≦θ≦360°, as shown in the following table 3.

                  TABLE 3                                                          ______________________________________                                         DIGITAL DATA  ANGLE θ°                                                                      sin θ                                                                               (cos θ)                             ______________________________________                                          0             0          0       1                                            .             .           .       .                                            .             .           .       .                                            .             .           .       .                                             30            30         0.5     0.85                                         .             .           .       .                                            .             .           .       .                                            .             .           .       .                                             90            90         1       0                                            .             .           .       .                                            .             .           .       .                                            .             .           .       .                                            150           150         0.5     -0.85                                        .             .           .       .                                            .             .           .       .                                            .             .           .       .                                            180           180         0       -1                                           .             .           .       .                                            .             .           .       .                                            .             .           .       .                                            210           210         -0.5    -0.85                                        .             .           .       .                                            .             .           .       .                                            .             .           .       .                                            270           270         -1      0                                            .             .           .       .                                            .             .           .       .                                            .             .           .       .                                            330           330         -0.5    0.85                                         .             .           .       .                                            .             .           .       .                                            .             .           .       .                                            360           360         0       1                                            ______________________________________                                    

In the case of the table 3, since current flowing direction can be set by adopting output terminals a₁ to b₂ of the drive circuits 6, 7 based on the sin θ (cos θ) data, the direction setting circuit 8 can be omitted. The cos θ data can be obtained from the sin θ data by shifting the phase of the sin θ, but the cos θ data may also be stored in the ROM.

Each of the pulse currents having duty ratios responsive to the detected variable can be generated from the sin θ duty pulse generator 4, and the cos θ duty pulse generator 5 in accordance with the sin 74 data and the cos θ data read from the ROM.

FIG. 8 shows the other embodiment of the cross coils type indicator according to the present invention. The indicator comprises a detection circuit 60 for detecting the amplitude of D.C. voltage from a frequency/voltage converter (F/V converter) 20 and a current control circuit 70 responsive to an output signal from the detection circuit 60 for controlling the amplitude of the pulse currents produced from an output circuit 50.

In FIG. 8, the same reference numerals indicate the same constructing elements as shown in FIG. 4. Namely, reference numeral 10 indicates a sensor for detecting a variable such as vehicle speed, engine speed and for producing a pulse signal, the frequency of which is responsive to the detected variable. Numeral 30 indicates a duty calculating circuit, 40 a duty pulse generating circuit, L₁ and L₂ cross coils, and Mg a magnet rotor.

In operation, a pulse signal is produced from the sensor 10 in accordance with the detected variable and it is applied to the F/V converter 20. The pulse signal is converted into a D.C. voltage by the F/V converter 20 and the output therefrom is applied to the detection circuit 60 on one hand, and to the duty calculating circuit 30 on the other hand. The detection circuit 60 detects the condition that whether or not actual rotational angles of the pointer responsive to the detected variable fall within a predetermined range of angles, e.g., between 0° and 10°, where the pointer A of the indicator has a possibility of contacting with the stopper pin P when the drive currents are initially applied to the cross coils L₁ and L₂, such as at a low range of angles of the pointer.

When the output signal from the F/V converter 20 do not fall within the predetermined range of angle, that is to say angle θ₁, pulse currents having duty ratios calculated by the duty calculating circuit 30 are produced from the duty pulse generating circuit 40 and the output from the detection circuit 60 causes the current control circuit 70 to operate. As a result, the current produced from the output circuit 50 has to be applied to the coils L₁ and L₂ to decrease.

FIG. 9 indicates the relationship between the pointer rotational angle θ and the pointer torque. As shown in FIG. 9, when the rotational angle θ of the pointer A falls within the range of the angle θ₁ where the pointer A may contact with the stopper pin P, the amplitude of the pulse currents to be applied to the coils L₁ and L₂ are reduced. As a result, the torque of the pointer A is decreased so that the mechanical force of the pointer A which tends to contact the pointer A with the stopper pin P is also weakened, thus preventing the generation of noises. Since the low indication area near zero indication has generally a low accuracy, the decrease in the torque causes no problem.

FIG. 10 shows another embodiment of the cross coil type indicator according to the present invention. In this embodiment, a microprocessor having a CPU (central processing unit), a RAM, and a ROM is used instead of the F/V converter 20, the duty calculation circuit 30 and the detection circuit 60 in FIG. 7. In this case, a pulse signal from the sensor 10 is directly applied to the microprocessor 80.

FIG. 11 shows a program flow chart of a control to be performed in the CPU of the microprocessor 80.

The operation of the CPU of the microprocessor 80 will now be made with reference to the flow chart of FIG. 11.

In step S₁, the frequency of the pulse signal from the sensor θ₁ is calculated and the operation moves to step S₂, where the rotational angle θ is calculated in accordance with the frequency. Then, the operation moves to step S₃, where the duty ratios of the pulse currents are calculated in accordance with sin θ and cos θ of the rotational angle θ and the operation now moves to step S₄.

In step S₄, a decision making is carried out about whether or not the duty ratios thus calculated are within a predetermined angle range θ₁. If the result of the decision is YES, that is, when the duty ratios are above the angle range θ, the operation moves to step S₅, where the duty pulses are generated from the duty pulse generating circuit 30 to the output circuit 50.

On the other hand, if the result of the decision in step S₄ is NO, that is, when the duty ratios are within the angle range θ₁, the operation moves to step S₆, where the current control circuit 70 is energized by an output signal from the microprocessor 80 and the amplitude of each pulse current to be produced from the output circuit 50 is reduced. As a result, the rotational torque of the pointer A is also reduced. It is to be noted in this case that the biasing force of the spiral spring C of the pointer A (see FIG. 1) has to be taken into consideration, when calculating the duty ratios corresponding to the rotational angle of the pointer A.

FIG. 12 indicates a detailed circuit of the output circuit 50 and the current control circuit 70 shown in FIGS. 8 and 10, according to the present invention. The construction of the control circuit 50 is same as the one shown in FIG. 6. Therefore, a detailed explanation of the function of the output circuit 50 will not be necessary.

In FIG. 12, the current control circuit 70 comprises a transistor Q₁ and a resistor R₁ connected in parallel between the power supply +Vcc and the input of the output circuit 50. The base of the transistor Q₁ is connected to the detection circuit 60 in FIG. 8 or to the microprocessor 80 in FIG. 10, and the collector and emitter of transistor Q₁ are connected through the resistor R₁.

In operation, when the rotational angle of the pointer A is above the predetermined angle θ₁, the output signal from either the detection circuit 60 or the microprocessor 80 is applied to the base of the transistor Q₁. Then, the transistor Q₁ is rendered conductive and the power supply+Vcc is directly connected to the output circuit 50. Accordingly, the circuit construction in this case becomes equivalent to the circuit construction shown in FIG. 6 and the pulse currents having the duty ratios corresponding to the rotational angle of the pointer A flow through the coils L₁ and L₂.

On the other hand, when the rotational angle of the pointer is within the predetermined angle θ₁, the output signal from either the detection circuit 60 or the microprocessor 80 is not applied to the base of the transistor Q₁. As a result, the transistor Q₁ is not rendered conductive, so that the resistor R₁ is inserted between the power supply +Vcc and the input of the output circuit 50. Consequently, the amplitude of the pulse currents i₁ and i₂ to be applied to the coils L₁ and L₂ are decreased, compared with the former case where the resistor R₁ is short-circuited or branched by the transistor Q₁, thus reducing the torque of the pointer A and preventing the noise from being generated.

FIG. 13 shows another embodiment of the cross coil type indicator according to the present invention. In this embodiment, when the rotational angle of the pointer A falls within the predetermined range of the angle θ, the duty ratios of the pulse currents to be applied to the coils L₁ and L₂ are reduced.

In FIG. 13, the cross coil type indicator comprises a detection circuit 60 and a current control circuit 70. The remaining construction elements such as sensor 10, F/V converter 20, duty calculation circuit 30, duty pulse generating circuit 40, output circuit 50 are the same as those shown in FIG. 8 and the same reference numerals are used thereto.

The input of the detection circuit 60 is connected to the output of the F/V converter 20, while the output of the detection circuit 60 is connected to the input of the current control circuit 70, so as to compensate for the duty ratios of pulse currents to be applied to the coils L₁ and L₂ in accordance with the output signal from the detection circuit 60.

In operation, the detection circuit 60 detects the output signal from the F/V converter 20, i.e., D.C. voltage responsive to a measured variable and determines if the rotational angle of the pointer A is within the predetermined range of angle θ, where the pointer A has a possibility of contacting with the stopper pin p (see FIG. 1).

When the rotational angle is above the predetermined range of angle θ₁, no output signal from the detection circuit 60 is produced and no compensation operation is performed to the duty ratios of the pulse currents to be applied to the coils L₁ and L₂ through the compensation circuit 70. Namely, the duty ratios calculated by the duty calculation circuit 30 is directly applied to the duty pulse generating circuit 40 without compensation and the pulse currents having the duty ratios without compensation generated by the circuit 40 are applied to the coils L₁ and L₂ through the output circuit 50.

On the other hand, when the rotational angle of the pointer A is within the predetermined range of angle θ₁, an output signal is produced from the detection circuit 60 and it is applied to the current control circuit 70. The duly ratios calculated by the duty calculation circuit 30 are multiplied by a predetermined coefficient β(0>β>1) and modified duty ratios thus multiplied are applied to the duty pulse generating circuit 40. As a result, the pulse currents having the modified duty ratios are generated from the circuit 40 and applied to the coils L₁ and L₂ through the output circuit 50. This means that the torque of the pointer A is decreased and the generation of the noise sound is prevented since the force which tends to contact the pointer A with the stopper pin p is weakened by the reduced torque.

In this case, since the same coefficient β is multiplied to the duty ratios of the pulse currents to be applied to the coils L₁ and L₂, the direction of the resultant magnetic field of the coils L₁ and L₂ becomes the same direction of the ones without compensation and no indication error occurs between the two cases.

FIG. 15 shows the relationship between the rotational angle θ of the pointer A and the duty ratios of the pulse currents to be applied to the coils L₁ and L₂ without compensation, while FIG. 16 shows the compensated or modified duty ratios of the pulse currents.

FIG. 14 shows still another embodiment of the cross coil type indicator according to the present invention.

In this embodiment, a microprocessor 80 having a CPU, a RAM, and a ROM is used instead of the F/V converter 20, the detection circuit 60, and the current control circuit 70 in FIG. 13. In FIG. 14, the same reference numerals shown in FIG. 13 are used to the same constructing elements.

The operation of the indicator shown in FIG. 14 will now be made with reference to a control flow chart shown in FIG. 17.

In step S₁ ^(a), frequency of a pulse signal from the sensor 10 is calculated and the operation moves to step S₂ ^(a), where a rotational angle θ is calculated in accordance with the frequency thus calculated.

Then, the duty ratios are calculated in accordance with sin θ and cos θ of the rotational angle θ in step S₃ ^(a) and the operation goes to step S₄ ^(a), where a decision is made about whether or not the duty ratios thus calculated are above a predetermined angle θ. If the result of the decision is YES, that is, the rotational angle θ is above the predetermined angle θ₁, the operation now goes to step S₅ ^(a), where duty pulses having duty ratios without compensation are generated by the duty pulse generating circuit 30 and they are applied to the coils L₁ and L₂ through the output circuit 50.

On the other hand, when the result of the decision in step S₄ ^(a) is NO, that is, the rotational angle 8 of the pointer A is within the predetermined range of angle θ₁, the operation moves to step S₆ ^(a), where the duty ratios thus calculated are multiplied by the coefficient β, and in step S₅ ^(a), pulse currents having the modified or compensated duty ratios are generated from the duty pulse generating circuit 30 and they are applied to the coils L₁ and L₂ through the output circuit 50.

It is to be noted in this case, however, that the biasing force of the spiral spring C of the pointer A (see FIG. 1) has to be taken into consideration when calculating the duty ratios.

As has been described about the embodiments, in the cross coil type indicator according to the present invention, a decision is made if the rotational angle of the pointer is within a predetermined range of angle θ₁, and when the rotational angle of the pointer above the predetermined angle θ₁, pulse currents having duty ratios without compensation are generated and are applied to the coils L₁ and L₂. On the other hand, when the rotational angle of the pointer is within the predetermined range of angle θ₁, pulse currents having compensated or modified duty ratios are generated and they are applied to the cross coils L₁ and L₂, thus reducing the torque of the pointer. As a result, the generation of the noise caused by the abutments between the pointer A and the stopper pin P can be prevented.

In the embodiments according to the present invention shown in FIGS. 8, 9, 13 and 14, the calculations of the duty ratios are shown as having been performed in either the duty calculation circuit 30 or the microprocessor 80. It is to be apparent for those skilled in the art that digital data corresponding to angles 8, and at least sin 8 may be stored in a ROM provided in the duty calculation circuit 30 or the ROM of the microprocessor 80 and each digital data corresponding to the rotational angle of the pointer A and its sin 8 can be read out of the ROM. The data corresponding to the cos 8 can also be obtained from the sin θ data by accessing to each memory location (θ+90°) of the ROM without storing data about cos 8, similar to the case shown in FIG. 7.

However, please note that the drive circuit for driving cross coils shown in FIG. 7 can be applied to the other cross coil type indicators besides the indicators shown in FIGS. 8, 9, 13 and 14.

While the invention has been described in its preferred embodiments, it is to be understood that the words which have been used are words of description rather than limitation and that various changes and modifications may be made within the purview of the appended claims without departing from the true scope and spirit of the invention in its broader aspects. 

What is claimed is:
 1. A cross coil type indicator, comprising:a pair of cross coils which are arranged so as to be mutually perpendicular; a magnetic rotor having a pointer at its center and rotatably provided within the coils, the magnetic rotor being adapted to be rotated by a resultant magnetic field which is generated by flowing pulse currents corresponding to a detected variable into the respective coils, thereby indicating the detected variable with an angular rotation of the magnetic rotor; means responsive to the detected variable for generating sin θ and cos θ data corresponding to an actual rotational angle θ of the magnetic rotor, wherein only the sin θ data within the range of φ≦θ≦90° is stored in the sin θ and cos θ data generating means; means for generating pulse currents each having a duty ratio in response to the sin θ and cos θ data output from the sin θ and cos θ data generating means, respectively, in which the data corresponding to a cos θ value is obtained from the data corresponding to the data of sin θ +90°, and sin θ and cos θ data values within the ranges of 90°≦θ180°, 180°≦θ≦270°, and 270°≦θ≦360° are obtained from the sin θ and cos θ data of φ°≦θ≦90°, respectively; output circuit means for driving the cross coils by flowing each of the pulse currents from the pulse current generating means to each coil; and direction setting means for changing through the output circuit means the directions of the pulse currents form the pulse current generating means which flow in the coils in accordance with each of the ranges of φ°≦θ≦0°, 90°≦θ≦180°, 180°≦θ≦270°, and 270°≦θ≦360°.
 2. The indicator as claimed in claim 1, wherein the sin θ and cos θ data generating means includes a Read Only Memory.
 3. The indicator as claimed in claim 1, further comprising a pin for restricting the rotational movement of the pointer at a predetermined position thereof, in which the indicator further comprises means for restraining from being produced contacting noise between the pointer and the stopper pin which is caused by the vibration of the pointer when the pointer is located in the vicinity of the stopper pin.
 4. The indicator as claimed in claim 3, wherein the restraining means comprises:means for detecting whether the rotational angle θ of the pointer comes into a predetermined range of angle θ₁ where the pointer has a possibility of contacting with the stopper pin and then outputting a detection signal; and means, which receives the detection signal and is dependent thereon, for reducing the amplitudes of the pulse currents to be supplied to the cross coils by controlling the output circuit means, when the rotational angle θ of the pointer comes into the predetermined angle θ, thereby reducing the rotational torque of the pointer to weaken contacting force of the pointer against the stopper pin.
 5. The indicator as claimed in claim 4, wherein the sin θ and cos θ data generating means and the detecting means includes a microprocessor.
 6. The indicator as claimed in claim 3, wherein the restraining means comprises:means for detecting whether the rotational angle θ of the pointer comes within a predetermined range of angle θ₁ where the pointer has a possibility of contacting the stopper pin and then outputting a detection signal; and means, which receives the detection signal and is dependent thereon, for compensating the duty ratios of the pulse currents form the pulse currents generating means which are to be supplied to the pulse currents generating means when the detecting means detects that actual the rotational angle θ of the pointer is within the predetermined range of angle θ₁, thereby reducing the rotational torque of the pointer to weaken contacting force of the pointer against the stopper pin.
 7. The indicator as claimed in claim 6, wherein the sin θ and cos θ data generating means, the detecting means and the compensating means are formed from a microprocessor. 